The deformational response of [+/- theta /90(4)](s) laminates under longitu
dinal tensile loading is treated by a synergistic approach that combines co
ntinuum damage mechanics (CDM) and micromechanics. The constraint of theta
degrees plies on transverse cracks in 90 degrees plies is represented by a
crack-opening displacement (COD) parameter in the CDM model and is expresse
d in terms of the ply properties and ply thickness ratios on the basis of a
finite-element calculation. A methodology is proposed for predicting the l
aminate stiffness variations with crack density and applied strain (or stre
ss) for various values of ply orientation B and is found to give good resul
ts. (C) 2001 Elsevier Science Ltd. All rights reserved.